View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 24278U 96046B 16269.80968445 -.00000053 00000-0 -14752-4 0 9999
2 24278 98.5820 181.8490 0349523 302.2159 54.5538 13.53071067993123
| Epoch (UTC): | 25 September 2016 19:25:56 |
| Eccentricity: | 0.0349523 |
| inclination: | 98.5820° |
| perigee height: | 801 km |
| apogee height: | 1321 km |
| right ascension of ascending node: | 181.8490° |
| argument of perigee: | 302.2159° |
| revolutions per day: | 13.53071067 |
| mean anomaly at epoch: | 54.5538° |
| orbit number at epoch: | 99312 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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